Photographic apparatus with mechanism to perform inclination correction

ABSTRACT

A photographic apparatus comprises a movable platform, an acceleration sensor, and a controller. 
     The movable platform has an imager that captures an optical image, and is movable and rotatable in an xy plane. The acceleration sensor detects a first gravitational component and a second gravitational component. The first gravitational component is the component of gravitational acceleration in the x direction. The second gravitational component is the component of gravitational acceleration in the y direction. The controller specifies a holding state of the photographic apparatus, calculates an inclination angle formed by rotation of the photographic apparatus, as measured with respect to a level plane, on the basis of the first and second gravitational components, and performs a movement control of the movable platform for an inclination correction based on the inclination angle. The controller specifies the holding state before an imaging operation, and performs the inclination correction during the imaging operation.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to a photographic apparatus, and in particular, to a photographic apparatus that performs an inclination correction.

2. Description of the Related Art

There is known a type of image stabilization (also known as anti-shake, but hereinafter, simply “stabilization”) apparatus for a photographic apparatus. The image stabilization apparatus corrects for the effects of hand shake by moving a movable platform including an image stabilization lens or by moving an imager (an imaging sensor) in an xy plane perpendicular to an optical axis of a taking lens of the photographic apparatus, in accordance with the amount of hand shake that occurs during the imaging process.

Japanese unexamined patent publication (KOKAI) No. 2006-71743 discloses an image stabilization apparatus that calculates hand-shake quantity on the basis of hand shake due to yaw, pitch, and roll, and then performs a stabilization on the basis of the hand-shake quantity (the first, second, and third hand-shake angles).

In this stabilization operation, the following stabilization functions are performed: a first stabilization that corrects the hand shake caused by yaw, a second stabilization that corrects the hand shake caused by pitch, and a third stabilization that corrects the hand shake caused by roll.

In the third stabilization, the rotation angle (hand shake displacement angle) of the photographic apparatus is calculated from the point when the third stabilization commences. However, the inclination angle of the photographic apparatus, formed by rotation of the photographic apparatus around its optical axis, as measured with respect to a level plane, is not considered. The inclination angle changes according to the orientation of the photographic apparatus.

If the photographic apparatus is inclined when the stabilization commences, the third stabilization is performed so as to keep this inclined state. Therefore, the inclination correction in order to level is not performed so that each of the four sides of the rectangle composing the outline of the imaging surface of the imager is not parallel to either the x direction or the y direction, in other words, the image is captured with the imager being inclined.

SUMMARY OF THE INVENTION

Therefore, an object of the present invention is to provide a photographic apparatus that performs the inclination correction.

According to the present invention, a photographic apparatus comprises a movable platform, an acceleration sensor, and a controller.

The movable platform has an imager that captures an optical image through a taking lens, and is movable and rotatable in an xy plane perpendicular to an optical axis of the taking lens.

The acceleration sensor detects a first gravitational component and a second gravitational component. The first gravitational component is the component of gravitational acceleration in the x direction perpendicular to the optical axis. The second gravitational component is the component of gravitational acceleration in the y direction perpendicular to the optical axis and the x direction.

The controller specifies a holding state of the photographic apparatus, calculates an inclination angle of the photographic apparatus formed by rotation of the photographic apparatus around the optical axis, as measured with respect to a level plane perpendicular to the direction of gravitational force, on the basis of the first gravitational component and the second gravitational component, and performs a movement control of the movable platform for an inclination correction based on the inclination angle.

The controller specifies the holding state before an imaging operation by the imager that commences when a shutter release switch is set to the ON state, and performs the inclination correction during the imaging operation.

BRIEF DESCRIPTION OF THE DRAWINGS

The objects and advantages of the present invention will be better understood from the following description, with reference to the accompanying drawings in which:

FIG. 1 is a perspective view of the embodiment of the photographic apparatus as viewed from the rear;

FIG. 2 is a front view of the photographic apparatus, when the photographic apparatus is held in the first horizontal orientation;

FIG. 3 is a circuit construction diagram of the photographic apparatus;

FIG. 4 is a flowchart that shows the main operation of the photographic apparatus;

FIG. 5 is a flowchart that shows the details of the timer interrupt process;

FIG. 6 illustrates the calculations involved in the stabilization and inclination correction;

FIG. 7 is a construction diagram of the movable platform;

FIG. 8 is a flowchart showing the details of the calculation of the third digital displacement angle;

FIG. 9 is a front view of the photographic apparatus, when the photographic apparatus is held in the second horizontal orientation;

FIG. 10 is a front view of the photographic apparatus, when the photographic apparatus is held in the first vertical orientation;

FIG. 11 is a front view of the photographic apparatus, when the photographic apparatus is held in the second vertical orientation;

FIG. 12 is a front view of the photographic apparatus, and Kθ_(n) is the angle formed when the photographic apparatus is rotated (inclined) in a counter-clockwise direction as viewed from the front, away from the first horizontal orientation;

FIG. 13 is a front view of the photographic apparatus, and Kθ_(n) is the angle formed when the photographic apparatus is rotated (inclined) in a counter-clockwise direction as viewed from the front, away from the first vertical orientation;

FIG. 14 is a front view of the photographic apparatus, and Kθ_(n) is the angle formed when the photographic apparatus is rotated (inclined) in a counter-clockwise direction as viewed from the front, away from the second horizontal orientation;

FIG. 15 is a front view of the photographic apparatus, and Kθ_(n) is the angle formed when the photographic apparatus is rotated (inclined) in a counter-clockwise direction as viewed from the front, away from the second vertical orientation;

FIG. 16 shows the first and second angle ranges; and

FIG. 17 is a flowchart showing the details of the calculation of the holding state parameter.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

The present invention is described below with reference to the embodiment shown in the drawings. In the embodiment, the photographic apparatus 1 is a digital camera. A camera lens (i.e. taking lens) 67 of the photographic apparatus 1 has the optical axis LX.

By way of orientation in the embodiment, the x direction, the y direction, and the z direction are defined (see FIG. 1). The x direction is the direction perpendicular to the optical axis LX. The y direction is the direction perpendicular to the optical axis LX and the x direction. The z direction is the direction parallel to the optical axis LX and perpendicular to both the x direction and the y direction.

The relationships between the direction of gravitational force and the x direction, the y direction, and the z direction, change according to the orientation of the photographic apparatus 1.

For example, when the photographic apparatus 1 is held in the first horizontal orientation, in other words, when the photographic apparatus 1 is held horizontally and the upper surface of the photographic apparatus 1 faces upward (see FIG. 2), the x direction and the z direction are perpendicular to the direction of gravitational force and the y direction is parallel to the direction of gravitational force.

When the photographic apparatus 1 is held in the second horizontal orientation, in other words, when the photographic apparatus 1 is held horizontally and the lower surface of the photographic apparatus 1 faces upward (see FIG. 9), the x direction and the z direction are perpendicular to the direction of gravitational force and the y direction is parallel to the direction of gravitational force.

When the photographic apparatus 1 is held in the first vertical orientation, in other words, when the photographic apparatus 1 is held vertically and one of the side surfaces of the photographic apparatus 1 faces upward (see FIG. 10), the x direction is parallel to the direction of gravitational force and the y direction and the z direction are perpendicular to the direction of gravitational force.

When the photographic apparatus 1 is held in the second vertical orientation, in other words, when the photographic apparatus 1 is held vertically and the other side surface of the photographic apparatus 1 faces upward (see FIG. 11), the x direction is parallel to the direction of gravitational force and the y direction and the z direction are perpendicular to the direction of gravitational force.

When the front surface of the photographic apparatus 1 faces in the direction of gravitational force, the x direction and the y direction are perpendicular to the direction of gravitational force and the z direction is parallel to the direction of gravitational force. The front surface of the photographic apparatus 1 is the side on which camera lens 67 is attached.

The imaging part of the photographic apparatus 1 comprises a PON button 11, a PON switch 11 a, a photometric switch 12 a, a shutter release button 13, a shutter release switch 13 a for an exposure operation, a correction button 14, a correction switch 14 a, a display 17 such as an LCD monitor or the like, a mirror-aperture-shutter unit 18, a DSP 19, a CPU 21, an AE (automatic exposure) unit 23, an AF (automatic focus) unit 24, an imaging unit 39 a in the correction unit 30, and the camera lens 67 (see FIGS. 1, 2, and 3).

Whether the PON switch 11 a is in the ON state or OFF state is determined by the state of the PON button 11. The ON/OFF states of the photographic apparatus 1 correspond to the ON/OFF states of the PON switch 11 a.

The subject image is captured as an optical image through the camera lens 67 by the imaging unit 39 a, and the captured image is displayed on the display 17. The subject image can be optically observed through the optical finder (not depicted).

When the shutter release button 13 is partially depressed by the operator, the photometric switch 12 a changes to the ON state so that the photometric operation, the AF sensing operation, and the focusing operation are performed.

When the shutter release button 13 is fully depressed by the operator, the shutter release switch 13 a changes to the ON state so that the imaging operation by the imaging unit 39 a (the imaging apparatus) is performed, and the captured image is stored.

The CPU 21 performs a release-sequence operation including the imaging operation after the shutter release switch 13 a is set to the ON state.

The mirror-aperture-shutter unit 18 is connected to port P7 of the CPU 21 and performs an UP/DOWN operation of the mirror (a mirror-up operation and a mirror-down operation), an OPEN/CLOSE operation of the aperture, and an OPEN/CLOSE operation of the shutter corresponding to the ON state of the shutter release switch 13 a.

The camera lens 67 is an interchangeable lens of the photographic apparatus 1 and is connected to port P8 of the CPU 21. The camera lens 67 outputs the lens information including the lens coefficient F etc., stored in a built-in ROM in the camera lens 67, to the CPU 21, when the photometric operation is performed.

The DSP 19 is connected to port P9 of the CPU 21 and to the imaging unit 39 a. Based on a command from the CPU 21, the DSP 19 performs the calculation operations, such as the image-processing operation, etc., on the image signal obtained by the imaging operation of the imaging unit 39 a.

The CPU 21 is a control apparatus that controls each part of the photographic apparatus 1 in its imaging operation, and in its stabilization (i.e. anti-shake) and inclination correction.

The stabilization and inclination correction includes both the movement control of the movable platform 30 a and position-detection efforts.

In the embodiment, the stabilization includes a first stabilization that moves the movable platform 30 a in the x direction and a second stabilization that moves the movable platform 30 a in the y direction.

Furthermore, the CPU 21 stores the value of the correction parameter SR that indicates whether the photographic apparatus 1 is in the correction mode or not, the value of the release-state parameter RP, the value of the mirror state parameter MP, and the value of the holding state parameter SIS.

The value of the release-state parameter RP changes with respect to the release-sequence operation. When the release-sequence operation is performed, the value of the release-state parameter RP is set to 1 (see steps S21 to S28 in FIG. 4), otherwise, the value of the release-state parameter RP is set (reset) to 0 (see steps S13 and S28 in FIG. 4).

While the mirror-up operation is performed before the exposure operation for the imaging operation, the value of the mirror state parameter MP is set to 1 (see step S22 in FIG. 4); otherwise, the value of the mirror state parameter MP is set to 0 (see step S24 in FIG. 4).

Whether the mirror-up operation of the photographic apparatus 1 is finished is determined by the detection of the ON/OFF states of a mechanical switch (not depicted). Whether the mirror-down operation of the photographic apparatus 1 is finished is determined by the detection of the completion of the shutter charge.

The holding state parameter SIS is the parameter whose value changes in accordance with the holding state of the photographic apparatus 1.

Specifically, when the photographic apparatus 1 is held approximately in the first horizontal orientation as shown in FIG. 2, the value of the holding state parameter SIS is set to 0 (SIS=0). When the photographic apparatus 1 is held approximately in the second horizontal orientation as shown in FIG. 9, the value of the holding state parameter SIS is set to 1 (SIS=1). When the photographic apparatus 1 is held approximately in the first vertical orientation as shown in FIG. 10, the value of the holding state parameter SIS is set to 2 (SIS=2). When the photographic apparatus 1 is held approximately in the second vertical orientation as shown in FIG. 11, the value of the holding state parameter SIS is set to 3 (SIS=3).

The holding state parameter SIS is used for the photometric operation (see step S18 in FIG. 4), the AF sensing operation (see step S19 in FIG. 4), and storing the image, on which the image-processing operation is performed, in the memory of the photographic apparatus 1 (see step S30 in FIG. 4).

Specifically, selecting and weighting of the photometric area are performed in accordance with the holding state of the photographic apparatus 1, in the photometric operation.

Furthermore, selecting and weighting of the AF sensing area are performed in accordance with the holding state of the photographic apparatus 1, in the AF sensing operation.

Information indicating that the photographic apparatus 1 is held approximately in which one of either the first horizontal orientation, the second horizontal orientation, the first vertical orientation, or the second vertical orientation, is attached to the header etc., of the file of the image that is stored in the memory.

Furthermore, the CPU 21 stores the values of the first digital angular velocity signal Vx_(n), the second digital angular velocity signal Vy_(n), the first digital angular velocity VVx_(n), the second digital angular velocity VVy_(n), the first digital acceleration signal Dah_(n), the second digital acceleration signal Dav_(n), the first digital acceleration Aah_(n), the second digital acceleration Aav_(n), the first digital displacement angle Kθ_(n) (the hand-shake angle caused by yaw), the second digital displacement angle Ky_(n) (the hand-shake angle caused by pitch), the third digital displacement angle Kθ_(n) (the inclination angle of the photographic apparatus 1), the horizontal direction component of the position S_(n), Sx_(n), the vertical direction component of the position S_(n), Sy_(n), the rotational direction component (the inclination angle) of the position S_(n), Sθ_(n), the first vertical direction component of the first driving point, Syl_(n), the second vertical direction component of the second driving point, Syr_(n), the horizontal driving force Dx_(n), the first vertical driving force Dyl_(n), the second vertical driving force Dyr_(n), the horizontal direction component of the position P_(n) after A/D conversion, pdx_(n), the first vertical direction component of the position P_(n) after A/D conversion, pdyl_(n), the second vertical direction component of the position P_(n) after A/D conversion, pdyr_(n), the lens coefficient F, and the hall sensor distance coefficient HSD. The hall sensor distance coefficient HSD is the relative distance between the first vertical hall sensor hv1 and the second vertical hall sensor hv2 in the x direction of the initial state (see FIG. 7).

In the initial state, the movable platform 30 a is positioned at the center of its movement range in both the x and y directions, and each of the four sides of the rectangle composing the outline of the imaging surface of the imager (an imaging sensor) 39 a 1 is parallel to either the x direction or the y direction.

The AE unit (exposure-calculating unit) 23 performs the photometric operation and calculates photometric values based on the subject being photographed. The AE unit 23 also calculates the aperture value and the duration of the exposure operation, with respect to the photometric values, both of which are needed for the imaging operation. The AF unit 24 performs the AF sensing operation and the corresponding focusing operation, both of which are needed for the imaging operation. In the focusing operation, the camera lens 67 is re-positioned along the optical axis LX.

The stabilization and inclination correction part (the stabilization and inclination correction apparatus) of the photographic apparatus 1 comprises a correction button 14, a correction switch 14 a, a display 17, a CPU 21, a detection unit 25, a driver circuit 29, a correction unit 30, a hall-sensor signal-processing unit 45, and the camera lens 67.

The ON/OFF states of the correction switch 14 a change according to the operation state of the correction button 14.

Specifically, when the correction button 14 is depressed by the operator, the correction switch 14 a is changed to the ON state so that the stabilization (the translational movement) and inclination correction, in which the detection unit 25 and the correction unit 30 are driven independently of the other operations which include the photometric operation etc., is carried out at the predetermined time interval. When the correction switch 14 a is in the ON state, (in other words in the correction mode), the correction parameter SR is set to 1 (SR=1). When the correction switch 14 a is not in the ON state, (in other words in the non-correction mode), the correction parameter SR is set to 0 (SR=0). In the embodiment, the value of the predetermined time interval is set to 1 ms.

The various output commands corresponding to the input signals of these switches are controlled by the CPU 21.

The information indicating whether the photometric switch 12 a is in the ON state or OFF state is input to port P12 of the CPU 21 as a 1-bit digital signal. The information indicating whether the shutter release switch 13 a is in the ON or OFF state is input to port P13 of the CPU 21 as a 1-bit digital signal. Likewise, the information indicating whether the correction switch 14 a is in the ON or OFF state is input to port P14 of the CPU 21 as a 1-bit digital signal.

The AE unit 23 is connected to port P4 of the CPU 21 for inputting and outputting signals. The AF unit 24 is connected to port P5 of the CPU 21 for inputting and outputting signals. The display 17 is connected to port P6 of the CPU 21 for inputting and outputting signals.

Next, the details of the input and output relationships between the CPU 21 and the detection unit 25, the driver circuit 29, the correction unit 30, and the hall-sensor signal-processing unit 45 are explained.

The detection unit 25 has a first angular velocity sensor 26 a, a second angular velocity sensor 26 b, an acceleration sensor 26 c, a first high-pass filter circuit 27 a, a second high-pass filter circuit 27 b, a first amplifier 28 a, a second amplifier 28 b, a third amplifier 28 c, and a fourth amplifier 28 d.

The first angular velocity sensor 26 a detects the angular velocity of rotary motion of the photographic apparatus 1 around the axis of the y direction (the yaw). In other words, the first angular velocity sensor 26 a is a gyro sensor that detects the yaw angular velocity.

The second angular velocity sensor 26 b detects the angular velocity of rotary motion of the photographic apparatus 1 around the axis of the x direction (the pitch). In other words, the second angular velocity sensor 26 b is a gyro sensor that detects the pitch angular velocity.

The acceleration sensor 26 c detects a first gravitational component and a second gravitational component. The first gravitational component is the horizontal component of gravitational acceleration in the x direction. The second gravitational component is the vertical component of gravitational acceleration in the y direction.

The first high-pass filter circuit 27 a reduces the low-frequency component of the signal output from the first angular velocity sensor 26 a, because the low-frequency component of the signal output from the first angular velocity sensor 26 a includes signal elements that are based on null voltage and panning motion, neither of which are related to hand shake.

Similarly, the second high-pass filter circuit 27 b reduces the low-frequency component of the signal output from the second angular velocity sensor 26 b, because the low-frequency component of the signal output from the second angular velocity sensor 26 b includes signal elements that are based on null voltage and panning motion, neither of which are related to hand shake.

The first amplifier 28 a amplifies the signal representing the yaw angular velocity, whose low-frequency component has been reduced, and outputs the analog signal to the A/D converter A/D 0 of the CPU 21 as a first angular velocity vx.

The second amplifier 28 b amplifies the signal representing the pitch angular velocity, whose low-frequency component has been reduced, and outputs the analog signal to the A/D converter A/D 1 of the CPU 21 as a second angular velocity vy.

The third amplifier 28 c amplifies the signal representing the first gravitational component output from the acceleration sensor 26 c, and outputs the analog signal to the A/D converter A/D 2 of the CPU 21 as a first acceleration ah.

The fourth amplifier 28 d amplifies the signal representing the second gravitational component output from the acceleration sensor 26 c, and outputs the analog signal to the A/D converter A/D 3 of the CPU 21 as a second acceleration av.

The third and fourth amplifiers 28 c and 28 d are connected to port P10 of the CPU 21. The amplification rate of the third and fourth amplifiers 28 c and 28 d are set on the basis of the output signal from port P10 of the CPU 21.

Specifically, the Hi signal is output to the third and fourth amplifiers 28 c and 28 d, in order to amplify the signal representing the first and second gravitational components with the low amplification rate Am2, and to calculate the holding state parameter SIS, until the release sequence operation commences.

The Lo signal is output to the third and fourth amplifiers 28 c and 28 d, in order to amplify the signal representing the first and second gravitational components with the high amplification rate Am1, and to perform the inclination correction, during the release sequence operation.

In the inclination correction, the movable platform 30 a is rotated within the movement range, but cannot be rotated beyond the movement range.

An angular range within which the inclination correction can be performed is defined as a first angle range θ_(inc).

An output range of the signal representing the first and second gravitational components corresponding to the first angle range θ_(inc) is defined as a first output range W1.

On the other hand, in the calculation of the holding state parameter SIS, it is necessary to consider the any type of the envisioned holding states of the photographic apparatus 1.

An angular range within which the inclination angle has to be detected for calculating the holding state parameter SIS is defined as a second angle range θ_(dec) (=90 degrees).

An output range of the signal representing the first and second gravitational components corresponding to the second angle range θ_(dec) is defined as a second output range W2.

The first angle range θ_(inc) is narrower than the second angle range θ_(dec) (θ_(inc)<θ_(dec), see FIG. 16).

Therefore, the first output range W1 is narrower than the second output range W2.

In the inclination correction, it is necessary to calculate the inclination angle (third digital displacement angle Kθ_(n)) accurately, in order to level the inclined movable platform 30 a. Namely, it is necessary to obtain the first and second accelerations ah and av with a high degree of accuracy.

On the other hand, in the calculation of the holding state parameter SIS, it is not necessary to calculate the inclination angle accurately, because the holding state parameter SIS is selected from the four numbers 0 to 3 corresponding to the orientation of the photographic apparatus 1.

In the inclination correction, the amplification for the signal representing the first and second gravitational components with the high amplification rate Am1 is performed by the third and fourth amplifiers 28 c and 28 d, in order to widen the narrow first output range W1 until it reaches the limit of the input range of the A/D converters A/D 2 and A/D 3 of the CPU 21 that the A/D conversion can be performed. Namely, the detection resolution of the A/D conversion in the A/D converters A/D 2 and A/D 3 of the CPU 21 is increased. The high amplification rate Am1 is higher than the low amplification rate Am2 (Am1>Am2).

On the other hand, in the calculation of the holding state parameter SIS, the amplification for the signal representing the first and second gravitational components with the low amplification rate Am2 is performed by the third and fourth amplifiers 28 c and 28 d, in order to widen the wide second output range W2 until it reaches the limit of the input range of the A/D converters A/D 2 and A/D 3 of the CPU 21 that the A/D conversion can be performed. Namely, the detection resolution of the A/D conversion in the A/D converters A/D 2 and A/D 3 of the CPU 21 is decreased compared to the detection resolution used in the inclination correction.

Because the inclination correction is performed during the release sequence operation and the calculation of the holding state parameter SIS is performed before the release sequence operation commences, the timing of the inclination correction and the timing of the calculation of the holding state parameter SIS do not overlap. Therefore, a problem does not occur, even if the amplification rate of the third and fourth amplifiers 28 c and 28 d is changed in each of the inclination correction and the calculation of the holding state parameter SIS.

The reduction of the low-frequency component is a two-step process. The primary part of the analog high-pass filtering is performed first by the first and second high-pass filter circuits 27 a and 27 b, followed by the secondary part of the digital high-pass filtering that is performed by the CPU 21.

The cut-off frequency of the secondary part of the digital high-pass filtering is higher than that of the primary part of the analog high-pass filtering.

In the digital high-pass filtering, the value of a first high-pass filter time constant hx and a second high-pass filter time constant hy can be easily changed.

The supply of electric power to the CPU 21 and each part of the detection unit 25 begins after the PON switch 11 a is set to the ON state (i.e. when the main power supply is set to the ON state). The calculation of a hand-shake quantity (the digital displacement angle Kx_(n) and the second digital displacement angle Ky_(n)) and an inclination angle (the third digital displacement angle Kθ_(n)) begins after the PON switch 11 a is set to the ON state.

The CPU 21 converts the first angular velocity vx, which is input to the A/D converter A/D 0, to a first digital angular velocity signal Vx_(n) (A/D conversion operation). It also calculates a first digital angular velocity VVx_(n) by reducing the low-frequency component of the first digital angular velocity signal Vx_(n) (the digital high-pass filtering) because the low-frequency component of the first digital angular velocity signal Vx_(n) includes signal elements that are based on null voltage and panning motion, neither of which are related to hand shake. It also calculates a first hand-shake quantity (a first hand-shake displacement angle around the y direction: a first digital displacement angle Kx_(n) caused by yaw) by integrating the first digital angular velocity VVx_(n) (the integration), for the first stabilization.

Similarly, the CPU 21 converts the second angular velocity vy, which is input to the A/D converter A/D 1, to a second digital angular velocity signal Vy_(n) (A/D conversion operation). It also calculates a second digital angular velocity VVy_(n) by reducing the low-frequency component of the second digital angular velocity signal Vy_(n) (the digital high-pass filtering) because the low-frequency component of the second digital angular velocity signal Vy_(n) includes signal elements that are based on null voltage and panning motion, neither of which are related to hand shake. It also calculates a second hand-shake quantity (a second hand-shake displacement angle around the x direction: a second digital displacement angle Ky_(n) caused by pitch) by integrating the second digital angular velocity VVy_(n) (the integration), for the second stabilization.

Furthermore, the CPU 21 converts the first acceleration ah, which is input to the A/D converter A/D 2, to a first digital acceleration signal Dah_(n) (A/D conversion operation). It also calculates a first digital acceleration Aah_(n) by reducing the high-frequency component of the first digital acceleration signal Dah_(n) (the digital low-pass filtering) in order to reduce the noise component in the first digital acceleration signal Dah_(n).

Similarly, the CPU 21 converts the second acceleration av, which is input to the A/D converter A/D 3, to a second digital acceleration signal Dav_(n) (A/D conversion operation). It also calculates a second digital acceleration Aav_(n) by reducing the high-frequency component of the second digital acceleration signal Dav_(n) (the digital low-pass filtering) in order to reduce the noise component in the second digital acceleration signal Dav_(n).

The CPU 21 also calculates the inclination angle (third digital displacement angle Kθ_(n)) of the photographic apparatus 1, formed by rotation of the photographic apparatus 1 around its optical axis LX, as measured with respect to a level plane perpendicular to the direction of gravitational force, on the basis of the magnitude relation between the absolute value of the first digital acceleration Aah_(n) and the absolute value of the second digital acceleration Aav_(n).

The inclination angle (the third digital displacement angle Kθ_(n)) of the photographic apparatus 1 changes according to the orientation of the photographic apparatus 1 and is measured with respect to one of the first horizontal orientation, the second horizontal orientation, the first vertical orientation, and the second vertical orientation. Therefore, the inclination angle of the photographic apparatus 1 is represented by the angle at which the x direction or the y direction intersects a level plane.

When one of the x direction and the y direction intersects a level plane at an angle of 0 degrees, and when the other of the x direction and the y direction intersects a level plane at an angle of 90 degrees, the photographic apparatus 1 is in a non-inclined state.

Thus, the CPU 21 and the detection unit 25 have a function for calculating the hand-shake quantity (the first and second hand-shake quantities) and the inclination angle.

The first digital acceleration Aah_(n) (the first gravitational component) and the second digital acceleration Aav_(n) (the second gravitational component) change according to the orientation of the photographic apparatus 1, and take values from −1 to +1.

For example, when the photographic apparatus 1 is held in the first horizontal orientation, in other words, when the photographic apparatus 1 is held horizontally and the upper surface of the photographic apparatus 1 faces upward (see FIG. 2), the first digital acceleration Aah_(n) is 0 and the second digital acceleration Aav_(n) is +1.

When the photographic apparatus 1 is held in the second horizontal orientation, in other words, when the photographic apparatus 1 is held horizontally and the lower surface of the photographic apparatus 1 faces upward (see FIG. 9), the first digital acceleration Aah_(n) is 0 and the second digital acceleration Aav_(n) is −1.

When the photographic apparatus 1 is held in the first vertical orientation, in other words, when the photographic apparatus 1 is held vertically and one of the side surfaces of the photographic apparatus 1 faces upward (see FIG. 10), the first digital acceleration Aah_(n) is +1 and the second digital acceleration Aav_(n) is 0.

When the photographic apparatus 1 is held in the second vertical orientation, in other words, when the photographic apparatus 1 is held vertically and the other side surface of the photographic apparatus 1 faces upward (see FIG. 11), the first digital acceleration Aah_(n) is −1 and the second digital acceleration Aav_(n) is 0.

When the front surface of the photographic apparatus 1 faces the direction of gravitational force or the opposite direction, in other words, when the front surface of the photographic apparatus 1 faces upward or downward, the first digital acceleration Aah_(n) and the second digital acceleration Aav_(n) are 0.

When the photographic apparatus 1 is rotated (inclined) at an angle Kθ_(n) in a counter-clockwise direction viewed from the front, from the first horizontal orientation (see FIG. 12), the first digital acceleration Aah_(n) is +sin(Kθ_(n)) and the second digital acceleration Aav_(n) is +cos(Kθ_(n)).

Therefore, the inclination angle (the third digital displacement angle Kθ_(n)) can be calculated by performing an arcsine transformation on the first digital acceleration Aah_(n) or by performing an arccosine transformation on the second digital acceleration Aav_(n).

However, while the absolute value of the inclination angle (the third digital displacement angle Kθ_(n)) is very small, in other words, nearly 0, the variation of the sine function is larger than that of the cosine function so that the inclination angle is best calculated by using the arcsine transformation rather than the arccosine transformation (Kθ_(n)=+Sin⁻¹(Aah_(n)), see step S76 in FIG. 8).

When the photographic apparatus 1 is rotated (inclined) at an angle Kθ_(n) in a counter-clockwise direction viewed from the front, from the first vertical orientation (see FIG. 13), the first digital acceleration Aah_(n) is +cos(Kθ_(n)) and the second digital acceleration Aav_(n) is −sin(Kθ_(n)).

Therefore, the inclination angle (the third digital displacement angle Kθ_(n)) can be calculated by performing an arccosine transformation on the first digital acceleration Aah_(n) or by performing an arcsine transformation on the second digital acceleration Aav_(n) and taking the negative.

However, while the absolute value of the inclination angle (the third digital displacement angle Kθ_(n)) is very small, in other words, nearly 0, the variation of the sine function is larger than that of the cosine function so that the inclination angle is best calculated by using the arcsine transformation rather than the arccosine transformation (Kθ_(n)=−Sin⁻¹(Aav_(n)), see step S73 in FIG. 8).

When the photographic apparatus 1 is rotated (inclined) at an angle Kθ_(n) in a counter-clockwise direction viewed from the front, from the second horizontal orientation (see FIG. 14), the first digital acceleration Aah_(n) is −sin(Kθ_(n)) and the second digital acceleration Aav_(n) is −cos(Kθ_(n)).

Therefore, the inclination angle (the third digital displacement angle Kθ_(n)) can be calculated by performing an arcsine transformation on the first digital acceleration Aah_(n) and taking the negative or by performing an arccosine transformation on the second digital acceleration Aav_(n) and taking the negative.

However, while the absolute value of the inclination angle (the third digital displacement angle Kθ_(n)) is very small, in other words, nearly 0, the variation of the sine function is larger than that of the cosine function so that the inclination angle is best calculated by using the arcsine transformation rather than the arccosine transformation (Kθ_(n)=−Sin⁻¹(Aah_(n)), see step S77 in FIG. 8).

When the photographic apparatus 1 is rotated (inclined) at an angle Kθ_(n) in a counter-clockwise direction viewed from the front, from the second vertical orientation (see FIG. 15), the first digital acceleration Aah_(n) is −cos(Kθ_(n)) and the second digital acceleration Aav_(n) is +sin(Kθ_(n)).

Therefore, the inclination angle (the third digital displacement angle Kθ_(n)) can be calculated by performing an arccosine transformation on the first digital acceleration Aah_(n) and taking the negative or by performing an arcsine transformation on the second digital acceleration Aav_(n).

However, while the absolute value of the inclination angle (the third digital displacement angle Kθ_(n)) is very small, in other words, is nearly 0, the variation of the sine function is larger than that of the cosine function so that the inclination angle is best calculated by using the arcsine transformation rather than the arccosine transformation (Kθ_(n)=+Sin⁻¹(Aav_(n)), see step S74 in FIG. 8).

When the front surface of the photographic apparatus 1 faces mostly upward or downward, the first digital acceleration Aah_(n) and the second digital acceleration Aav_(n) are nearly 0. In this case, this means that inclination correction, in other words, the rotational movement in accordance with the inclination angle, is not necessary, it is desirable to perform the stabilization and inclination correction with the inclination angle being minimal.

However, when the arccosine transformation on the first digital acceleration Aah_(n) or the second digital acceleration Aav_(n) that is nearly 0 is performed, the absolute value of the inclination angle (the third digital displacement angle Kθ_(n)) is a large value. In this case, the stabilization and inclination correction is performed with the inclination angle being large, even when the rotational movement in accordance with the inclination angle is not necessary. Therefore, the inclination correction cannot be performed correctly.

Therefore, in order to eliminate the inclination angle, it is necessary to determine whether the front surface of the photographic apparatus 1 faces mostly upward or downward using an additional determination factor.

An example of the additional determination factor is the determination of whether the sum of the absolute value of the first digital acceleration Aah_(n) and the absolute value of the second digital acceleration Aav_(n) is less than a threshold value.

On the other hand, when the arcsine transformation on the first digital acceleration Aah_(n) or the second digital acceleration Aav_(n) that is nearly 0 is performed, the absolute value of the inclination angle (the third digital displacement angle Kθ_(n)) is a small value (nearly 0). In this case, the stabilization and inclination correction can be performed, with the inclination angle being small. Therefore, it is not necessary to determine whether the front surface of the photographic apparatus 1 faces mostly upward or downward by using the additional determination factor.

Furthermore, in the embodiment, the holding state of the photographic apparatus 1 is specified, on the basis of the magnitude relation between the absolute value of the first digital acceleration Aah_(n) and the absolute value of the second digital acceleration Aav_(n), and the sign of that larger value without applying the absolute value.

Specifically, when the absolute value of the second digital acceleration Aav_(n) is greater than or equal to the absolute value of the first digital acceleration Aah_(n), and when the second digital acceleration Aav_(n) is greater than or equal to 0, it is determined that the photographic apparatus 1 is held approximately in the first horizontal orientation (SIS=0, see step S96 in FIG. 17).

When the absolute value of the second digital acceleration Aav_(n) is greater than or equal to the absolute value of the first digital acceleration Aah_(n), and when the second digital acceleration Aav_(n) is less than 0, it is determined that the photographic apparatus 1 is held approximately in the second horizontal orientation (SIS=1, see step S97 in FIG. 17).

Specifically, when the absolute value of the second digital acceleration Aav_(n) is less than the absolute value of the first digital acceleration Aah_(n), and when the first digital acceleration Aah_(n) is greater than or equal to 0, it is determined that the photographic apparatus 1 is held approximately in the first vertical orientation (SIS=2, see step S93 in FIG. 17).

When the absolute value of the second digital acceleration Aav_(n) is less than the absolute value of the first digital acceleration Aah_(n), and when the first digital acceleration Aah_(n) is less than 0, it is determined that the photographic apparatus 1 is held approximately in the second vertical orientation (SIS=3, see step S94 in FIG. 17).

The value “n” is an integer greater than or equal to 0, and indicates the duration in milliseconds from the point when the timer interrupt process commences, (t=0, and see step S11 in FIG. 4), to when the last interrupt process of the timer is performed (t=n).

In the digital high-pass filtering regarding the yaw, the first digital angular velocity VVx_(n) is calculated by dividing the sum of the first digital angular velocity VVx₀ and VVx_(n-1) (calculated by the timer interrupt process before the 1 ms predetermined time interval, before the last timer interrupt process is performed) by the first high-pass filter time constant hx, and then subtracting the resulting quotient from the first digital angular velocity signal Vx_(n) (VVx_(n)=Vx_(n)−(ΣVVx_(n-1))÷hx, see (1) in FIG. 6).

In the digital high-pass filtering regarding the pitch, the second digital angular velocity VVy_(n) is calculated by dividing the sum of the second digital angular velocity VVy₀ and VVy_(n-1) (calculated by the timer interrupt process before the 1 ms predetermined time interval, before the last timer interrupt process is performed) by the second high-pass filter time constant hy, and then subtracting the resulting quotient from the second digital angular velocity signal Vy_(n) (VVy_(n)=Vy_(n)−(ΣVVy_(n-1))÷hy, see (1) in FIG. 6).

In the integration regarding the yaw, the first digital displacement angle Kθ_(n) is calculated by summing the first digital angular velocity VVx₀ at the point when the timer interrupt process commences, t=0, (see step S11 in FIG. 4) and the first digital angular velocity VVx_(n) at the point when the last timer interrupt process is performed (t=n), (Kx_(n)=ΣVVx_(n), see (7) in FIG. 6).

Similarly, in the integration regarding the pitch, the second digital displacement angle Ky_(n) is calculated by summing the second digital angular velocity VVy₀ at the point when the timer interrupt process commences and the second digital angular velocity VVy_(n) at the point when the last timer interrupt process is performed (Ky_(n)=ΣVVy_(n), see (7) in FIG. 6).

The inclination angle, in other words, the third digital displacement angle Kθ_(n) is calculated by performing the arcsine transformation on the smaller of the absolute value of the first digital acceleration Aah_(n) and the absolute value of the second digital acceleration Aav_(n) and by adding a positive or negative sign (Kθ_(n)=+Sin⁻¹(Aah_(n)), −Sin⁻¹(Aah_(n)), +Sin⁻¹(Aav_(n)), or −Sin⁻¹(Aav_(n)), see (8) in FIG. 6).

Whether the positive or negative sign is added is determined on the basis of the larger of the absolute value of the first digital acceleration Aah_(n) and the absolute value of the second digital acceleration Aav_(n), and the sign of that larger value without applying the absolute value (see steps S72 and S75 in FIG. 8).

In the embodiment, the angular velocity and acceleration detection operation during the timer interrupt process includes a process in the detection unit 25 and the input of the first angular velocity vx, the second angular velocity vy, the first acceleration ah, and the second acceleration av from the detection unit 25 to the CPU 21.

In the calculation of the third digital displacement angle Kθ_(n), an integration is not performed because it is unnecessary. Therefore, the DC offset does not affect the calculation of the third digital displacement angle Kθ_(n), so the inclination angle can be calculated accurately.

When the integration including the DC offset is used, the third digital displacement angle Kθ_(n) represents an unspecified value even if the inclination angle is 0. Accordingly, the movable platform 30 a including the imager 39 a 1 is rotated (inclined) compared to the initial state in order to correct the third digital displacement angle Kθ_(n) representing the unspecified value.

Because the displacement of the movable platform 30 a in this case means the inclination of the imager 39 a 1, the captured image displayed on the display 17 is inclined. When the operator sees the inclined image on the display 17, the operator must visually detect the inclination of the displayed image even if the inclination is very small.

However, in the embodiment, because the DC offset does not exist, the inclination of the imager 39 a 1 caused by the DC offset does not exist.

The CPU 21 calculates the position S_(n) where the imaging unit 39 a (the movable platform 30 a) should be moved, in accordance with the hand-shake quantity (the first and second digital displacement angles Kx_(n) and Ky_(n)) and the inclination angle (the third digital displacement angle Kθ_(n)) calculated for the x direction, the y direction, and the rotational direction, based on the lens coefficient F and the hall sensor distance coefficient HSD (Sx_(n)=F×tan(Kx_(n)), Sy_(n)=F×tan(Ky_(n)), and Sθ_(n)=HSD÷2×sin(Kθ_(n))). In this calculation, both the translational (linear) movement of the movable platform 30 a in the xy plane and the rotational movement of the movable platform 30 a in the xy plane are considered.

The horizontal direction component of the position S_(n) is defined as Sx_(n), the vertical direction component of the position S_(n) is defined as Sy_(n), and the rotational (inclination) direction component of the position S_(n) is defined as Sθ_(n).

The rotation of the movable platform 30 a is performed by applying different forces in the y direction on a first driving point and a second driving point on the movable platform 30 a. The movement of the movable platform 30 a in the y direction is performed by applying the same driving forces in the y direction on the first and second driving points on the movable platform 30 a. The first driving point is the point to which a first vertical electro-magnetic force based on the first vertical coil 32 a 1 is applied. The second driving point is the point to which a second vertical electro-magnetic force based on the second vertical coil 32 a 2 is applied. The first driving point is set to a position close to the first vertical hall sensor hv1. The second driving point is set to a position close to the second vertical hall sensor hv2.

The first vertical direction component of the first driving point corresponding to the position S_(n) is defined as Syl_(n). The second vertical direction component of the second driving point corresponding to the position S_(n) is defined as Syr_(n).

The first vertical direction component of the first driving point, Syl_(n), and the second vertical direction component of the second driving point, Syr_(n), are calculated on the basis of the vertical direction component of the position S_(n), Sy_(n), and the rotational direction component of the position S_(n), Sθ_(n), (Syl_(n)=Sy_(n)+Sθ_(n), Syr_(n)=Sy_(n)−Sθ_(n), see (4) in FIG. 6).

The calculations of the first digital displacement angle Kx_(n), the second digital displacement angle Ky_(n), the third digital displacement angle Kθ_(n), the rotational direction component of the position S_(n), Sθ_(n), the horizontal direction component of the position S_(n), Sx_(n), the vertical direction component of the position S_(n), Sy_(n), the first vertical direction component of the first driving point, Syl_(n), and the second vertical direction component of the second driving point, Syr_(n) are performed only when the correction parameter SR is set to 1 and during the release-sequence operation (see steps S62 to S65 of FIG. 5). The release-sequence operation commences after the shutter release button 13 is fully depressed and the shutter release switch 13 a is set to the ON state, and does not finish until the release-state parameter RP is set to 0.

When the stabilization and inclination correction is not performed (SR=0) and during the release sequence operation (RP=1), the position S_(n) (Sx_(n), Syl_(n), Syr_(n)) where the movable platform 30 a should be moved is set to the initial state (see step S61 in FIG. 5, Sx_(n)=Syl_(n)=Syr_(n)=0).

While the release-state parameter RP is set to 0, in other words, except for during the release sequence operation, the calculations of the first digital displacement angle Kx_(n), the second digital displacement angle Ky_(n), the third digital displacement angle Kθ_(n), the rotational direction component of the position S_(n), Sθ_(n), the horizontal direction component of the position S_(n), Sx_(n), the vertical direction component of the position S_(n), Sy_(n), the first vertical direction component of the first driving point, Syl_(n), and the second vertical direction component of the second driving point, Syr_(n) are not performed. Therefore, in this case, driving of the movable platform 30 a is not performed (see step S58 in FIG. 5).

However, the calculation of the holding state parameter SIS, which specifies the holding state of the photographic apparatus 1, is performed (see step S56 in FIG. 5).

Therefore, in the embodiment, the detection of the gravitational components for the inclination correction and for specifying the holding state of the photographic apparatus 1 can be performed by using the same acceleration sensor 26 c.

The movement of the movable platform 30 a, which includes the imaging unit 39 a, is performed by using an electro-magnetic force and is described later.

The driving force D_(n) is for driving the driver circuit 29 in order to move the movable platform 30 a to the position S_(n).

The horizontal direction component of the driving force D_(n) for the first and second horizontal coils 31 a 1 and 31 a 2 is defined as the horizontal driving force Dx_(n) (after D/A conversion, the horizontal PWM duty dx).

The vertical direction component of the driving force D_(n) for the first vertical coil 32 a 1 is defined as the first vertical driving force Dyl_(n) (after D/A conversion, the first vertical PWM duty dyl).

The vertical direction component of the driving force D_(n) for the second vertical coil 32 a 2 is defined as the second vertical driving force Dyr_(n) (after D/A conversion, the second vertical PWM duty dyr).

The correction unit 30 is an apparatus that corrects for the effects of hand shake by moving the imaging unit 39 a to the position S_(n), by canceling the lag of the subject image on the imaging surface of the imager 39 a 1 of the imaging unit 39 a, and by stabilizing the subject image displayed on the imaging surface of the imager 39 a 1.

The correction unit 30 has a fixed unit 30 b and a movable platform 30 a that includes the imaging unit 39 a and can be moved in the xy plane.

By moving the movable platform 30 a in the x direction, the first stabilization for correcting the hand shake caused by yaw, which is the first hand-shake displacement angle around the y direction, is performed; and by moving the movable platform 30 a in the y direction, the second stabilization for correcting the hand shake caused by pitch, which is the second hand-shake displacement angle around the x direction, is performed (the translational movement).

Moreover, the correction unit 30 performs the inclination correction (the rotational movement) that corrects (reduces) the inclination of the photographic apparatus 1 formed by rotation of the photographic apparatus 1 around its optical axis LX, as measured with respect to a level plane perpendicular to the direction of gravitational force, by rotating the movable platform 30 a including the imaging unit 39 a around an axis parallel to the optical axis LX.

In other words, in the inclination correction, the movement control repositions the movable platform 30 a so that the upper and lower sides of the rectangle composing the outline of the imaging surface of the imager 39 a 1 are perpendicular to the direction of gravitational force and the left and right sides are parallel to the direction of gravitational force.

Therefore, the imager 39 a 1 can be automatically leveled without using a level vial. When the photographic apparatus 1 images a subject including the horizon, the imaging operation can be performed, with the upper and lower sides of the rectangle composing the outline of the imaging surface of the imager 39 a 1 being parallel to the horizon.

Moreover, due to the inclination correction, the upper and lower sides of the rectangle composing the outline of the imaging surface of the imager 39 a 1 are kept perpendicular to the direction of gravitational force, and the left and right sides of the rectangle composing the outline of the imaging surface of the imager 39 a 1 are kept parallel to the direction of gravitational force. Therefore, hand shake caused by roll is also corrected by the inclination correction. In other words, rotating the movable platform 30 a in the xy plane for the inclination correction also achieves a third stabilization for correcting the hand shake caused by roll.

When the stabilization and inclination correction is not performed (SR=0), in other words, when the photographic apparatus 1 is not in the correction mode, the position S_(n) (Sx_(n), Syl_(n), Syr_(n)) where the movable platform 30 a should be moved is set to the predetermined position. In the embodiment, the predetermined position is the center of its movement range.

Driving of the movable platform 30 a, including movement to the fixed (held) position of the initial state, is performed by the electro-magnetic force of the coil unit and the magnetic unit through the driver circuit 29, which has the horizontal PWM duty dx input from the PWM 0 of the CPU 21, the first vertical PWM duty dyl input from the PWM 1 of the CPU 21, and the second vertical PWM duty dyr input from the PWM 2 of the CPU 21 (see (6) in FIG. 6).

The detected-position P_(n) of the movable platform 30 a, either before or after the movement effected by the driver circuit 29, is detected by the hall sensor unit 44 a and the hall-sensor signal-processing unit 45.

Information regarding the horizontal direction component of the detected-position P_(n), in other words, the horizontal detected-position signal px, is input to the A/D converter A/D 4 of the CPU 21 (see (2) in FIG. 6). The horizontal detected-position signal px is an analog signal that is converted to a digital signal by the A/D converter A/D 4 (A/D conversion operation). The horizontal direction component of the detected-position P_(n) after the A/D conversion operation, is defined as pdx_(n) and corresponds to the horizontal detected-position signal px.

Information regarding one of the vertical direction components of the detected-position P_(n), in other words, the first vertical detected-position signal pyl, is input to the A/D converter A/D 5 of the CPU 21. The first vertical detected-position signal pyl is an analog signal that is converted to a digital signal by the A/D converter A/D 5 (A/D conversion operation). The first vertical direction component of the detected-position P_(n) after the A/D conversion operation is defined as pdyl_(n) and corresponds to the first vertical detected-position signal pyl.

Information regarding the other of the vertical direction components of the detected-position P_(n), in other words, the second vertical detected-position signal pyr, is input to the A/D converter A/D 6 of the CPU 21. The second vertical detected-position signal pyr is an analog signal that is converted to a digital signal by the A/D converter A/D 6 (A/D conversion operation). The second vertical direction component of the detected-position P_(n) after the A/D conversion operation is defined as pdyr_(n) and corresponds to the second vertical detected-position signal pyr.

The PID (Proportional Integral Differential) control calculates the horizontal driving force Dx_(n) and the first and second vertical driving forces Dyl_(n) and Dyr_(n) on the basis of the coordinate data for the detected-position P_(n) (pdx_(n), pdyl_(n), pdyr_(n)) and the position S_(n) (Sx_(n), Syl_(n), Syr_(n)) following movement (see (5) in FIG. 6).

Driving of the movable platform 30 a to the position S_(n), (Sx_(n), Syl_(n), Syr_(n)) corresponding to the stabilization and inclination correction of the PID control, is performed when the photographic apparatus 1 is in the correction mode (SR=1) where the correction switch 14 a is set to the ON state and when the release-state parameter RP is set to 1 (RP=1).

When the correction parameter SR is 0 and the release-state parameter RP is set to 1, PID control unrelated to the stabilization and inclination correction is performed so that the movable platform 30 a is moved to the predetermined position (the center of the movement range) at the initial state such that each of the four sides composing the outline of the imaging surface of the imager 39 a 1 of the imaging unit 39 a is parallel to either the x direction or the y direction, in other words, such that the movable platform 30 a is not rotated (inclined).

The movable platform 30 a has a coil unit for driving that is comprised of a first horizontal coil 31 a 1, a second horizontal coil 31 a 2, a first vertical coil 32 a 1, and a second vertical coil 32 a 2, an imaging unit 39 a having the imager 39 a 1, and a hall sensor unit 44 a as a magnetic-field change-detecting element unit (see FIG. 7). In the embodiment, the imager 39 a 1 is a CCD; however, the imager 39 a 1 may be of another type, such as a CMOS, etc.

The fixed unit 30 b has a magnetic position detection and driving unit that is comprised of a first horizontal magnet 411 b 1, a second horizontal magnet 411 b 2, a first vertical magnet 412 b 1, a second vertical magnet 412 b 2, a first horizontal yoke 431 b 1, a second horizontal yoke 431 b 2, a first vertical yoke 432 b 1, and a second vertical yoke 432 b 2.

The fixed unit 30 b movably and rotatably supports the movable platform 30 a in the rectangular-shaped movement range in the xy plane, using balls, etc. The balls are arranged between the fixed unit 30 b and the movable platform 30 a.

When the central area of the imager 39 a 1 is intersecting the optical axis LX of the camera lens 67, the relationship between the position of the movable platform 30 a and the position of the fixed unit 30 b is arranged so that the movable platform 30 a is positioned at the center of its movement range in both the x direction and the y direction, in order to utilize the full size of the imaging range of the imager 39 a 1.

The rectangular form of the imaging surface of the imager 39 a 1 has two diagonal lines. In the embodiment, the center of the imager 39 a 1 is at the intersection of these two diagonal lines.

Furthermore, the movable platform 30 a is positioned at the center of its movement range in both the x direction and the y direction, and each of the four sides composing the outline of the imaging surface of the imager 39 a 1 is parallel to either the x direction or the y direction, in the initial state immediately after the shutter release switch 13 a is set to the ON state so that the release sequence operation commences (see step S21 of FIG. 4). Then, the stabilization and inclination correction commences.

The first horizontal coil 31 a 1, the second horizontal coil 31 a 2, the first vertical coil 32 a 1, the second vertical coil 32 a 2, and the hall sensor unit 44 a are attached to the movable platform 30 a.

The first horizontal coil 31 a 1 forms a seat and a spiral-shaped coil pattern. The coil pattern of the first horizontal coil 31 a 1 has lines which are parallel to the y direction, thus creating the first horizontal electro-magnetic force to move the movable platform 30 a that includes the first horizontal coil 31 a 1, in the x direction.

The first horizontal electro-magnetic force is created by the current direction of the first horizontal coil 31 a 1 and the magnetic-field direction of the first horizontal magnet 411 b 1.

The second horizontal coil 31 a 2 forms a seat and a spiral-shaped coil pattern. The coil pattern of the second horizontal coil 31 a 2 has lines which are parallel to the y direction, thus creating the second horizontal electro-magnetic force to move the movable platform 30 a that includes the second horizontal coil 31 a 2, in the x direction.

The second horizontal electro-magnetic force is created by the current direction of the second horizontal coil 31 a 2 and the magnetic-field direction of the second horizontal magnet 411 b 2.

The first vertical coil 32 a 1 forms a seat and a spiral-shaped coil pattern. The coil pattern of the first vertical coil 32 a 1 has lines which are parallel to the x direction, thus creating the first vertical electro-magnetic force to move the movable platform 30 a that includes the first vertical coil 32 a 1, in the y direction and to rotate the movable platform 30 a.

The first vertical electro-magnetic force is created by the current direction of the first vertical coil 32 a 1 and the magnetic-field direction of the first vertical magnet 412 b 1.

The second vertical coil 32 a 2 forms a seat and a spiral-shaped coil pattern. The coil pattern of the second vertical coil 32 a 2 has lines which are parallel to the x direction, thus creating the second vertical electro-magnetic force to move the movable platform 30 a that includes the second vertical coil 32 a 2, in the y direction and to rotate the movable platform 30 a.

The second vertical electro-magnetic force is created by the current direction of the second vertical coil 32 a 2 and the magnetic-field direction of the second vertical magnet 412 b 2.

The first and second horizontal coils 31 a 1 and 31 a 2 and the first and second vertical coils 32 a 1 and 32 a 2 are connected to the driver circuit 29, which drives the first and second horizontal coils 31 a 1 and 31 a 2 and the first and second vertical coils 32 a 1 and 32 a 2, through the flexible circuit board (not depicted).

The horizontal PWM duty dx, that is a duty ratio of a PWM pulse, is input to the driver circuit 29 from the PWM 0 of the CPU 21. The first vertical PWM duty dyl, that is a duty ratio of a PWM pulse, is input to the driver circuit 29 from the PWM 1 of the CPU 21. The second vertical PWM duty dyr, that is a duty ratio of a PWM pulse, is input to the driver circuit 29 from the PWM 2 of the CPU 21.

The driver circuit 29 supplies the same power to the first and second horizontal coils 31 a 1 and 31 a 2, corresponding to the value of the horizontal PWM duty dx, to move the movable platform 30 a in the x direction.

The driver circuit 29 supplies power to the first vertical coil 32 a 1 corresponding to the value of the first vertical PWM duty dyl and to the second vertical coil 32 a 2 corresponding to the value of the second vertical PWM duty dyr, in order to move the movable platform 30 a in the y direction and to rotate the movable platform 30 a.

The positional relationship between the first and second horizontal coils 31 a 1 and 31 a 2 is determined so that the optical axis LX is located between the first and second horizontal coils 31 a 1 and 31 a 2 in the x direction, in the initial state. In other words, the first and second horizontal coils 31 a 1 and 31 a 2 are arranged in a symmetrical arrangement centered on the optical axis LX, in the x direction in the initial state.

The first and second vertical coils 32 a 1 and 32 a 2 are arranged in the x direction in the initial state.

The first and second horizontal coils 31 a 1 and 31 a 2 are arranged such that the distance between the central area of the imager 39 a 1 and the central area of the first horizontal coil 31 a 1 in the x direction is the same as the distance between the center of the imager 39 a 1 and the central area of the second horizontal coil 31 a 2 in the x direction.

The first and second vertical coils 32 a 1 and 32 a 2 are arranged such that in the initial state, the distance between the central area of the imager 39 a 1 and the central area of the first vertical coil 32 a 1 in the y direction is the same as the distance between the center of the imager 39 a 1 and the central area of the second vertical coil 32 a 2 in the y direction.

The first horizontal magnet 411 b 1 is attached to the movable platform side of the fixed unit 30 b, where the first horizontal magnet 411 b 1 faces the first horizontal coil 31 a 1 and the horizontal hall sensor hh10 in the z direction.

The second horizontal magnet 411 b 2 is attached to the movable platform side of the fixed unit 30 b, where the second horizontal magnet 411 b 2 faces the second horizontal coil 31 a 2 in the z direction.

The first vertical magnet 412 b 1 is attached to the movable platform side of the fixed unit 30 b, where the first vertical magnet 412 b 1 faces the first vertical coil 32 a 1 and the first vertical hall sensor hv1 in the z direction.

The second vertical magnet 412 b 2 is attached to the movable platform side of the fixed unit 30 b, where the second vertical magnet 412 b 2 faces the second vertical coil 32 a 2 and the second vertical hall sensor hv2 in the z direction.

The first horizontal magnet 411 b 1 is attached to the first horizontal yoke 431 b 1, such that the N pole and S pole are arranged in the x direction. The first horizontal yoke 431 b 1 is attached to the fixed unit 30 b.

Likewise, the second horizontal magnet 411 b 2 is attached to the second horizontal yoke 431 b 2, such that the N pole and S pole are arranged in the x direction. The second horizontal yoke 431 b 2 is attached to the fixed unit 30 b.

The first vertical magnet 412 b 1 is attached to the first vertical yoke 432 b 1, such that the N pole and S pole are arranged in the y direction. The first vertical yoke 432 b 1 is attached to the fixed unit 30 b.

Likewise, the second vertical magnet 412 b 2 is attached to the second vertical yoke 432 b 2, such that the N pole and S pole are arranged in the y direction. The second vertical yoke 432 b 2 is attached to the fixed unit 30 b.

The first and second horizontal yokes 431 b 1 and 431 b 2 are made of a soft magnetic material.

The first horizontal yoke 431 b 1 prevents the magnetic field of the first horizontal magnet 411 b 1 from dissipating to the surroundings, and raises the magnetic-flux density between the first horizontal magnet 411 b 1 and the first horizontal coil 31 a 1, and between the first horizontal magnet 411 b 1 and the horizontal hall sensor hh10.

Similarly, the second horizontal yoke 431 b 2 prevents the magnetic field of the second horizontal magnet 411 b 2 from dissipating to the surroundings, and raises the magnetic-flux density between the second horizontal magnet 411 b 2 and the second horizontal coil 31 a 2.

The first and second vertical yokes 432 b 1 and 432 b 2 are made of a soft magnetic material.

The first vertical yoke 432 b 1 prevents the magnetic field of the first vertical magnet 412 b 1 from dissipating to the surroundings, and raises the magnetic-flux density between the first vertical magnet 412 b 1 and the first vertical coil 32 a 1, and between the first vertical magnet 412 b 1 and the first vertical hall sensor hv1.

Likewise, the second vertical yoke 432 b 2 prevents the magnetic field of the second vertical magnet 412 b 2 from dissipating to the surroundings, and raises the magnetic-flux density between the second vertical magnet 412 b 2 and the second vertical coil 32 a 2, and between the second vertical magnet 412 b 2 and the second vertical hall sensor hv2.

The first and second horizontal yokes 431 b 1 and 431 b 2 and the first and second vertical yokes 432 b 1 and 432 b 2 may be composed of one body or separate bodies.

The hall sensor unit 44 a is a one-axis hall sensor with three component hall sensors that are electromagnetic converting elements (magnetic-field change-detecting elements) using the Hall Effect. The hall sensor unit 44 a detects the horizontal detected-position signal px, the first vertical detected-position signal pyl, and the second vertical detected-position signal pyr.

One of the three hall sensors is a horizontal hall sensor hh10 for detecting the horizontal detected-position signal px, and another of the three hall sensors is a first vertical hall sensor hv1 for detecting the first vertical detected-position signal pyl, with the third being a second vertical hall sensor hv2 for detecting the second vertical detected-position signal pyr.

The horizontal hall sensor hh10 is attached to the movable platform 30 a, where the horizontal hall sensor hh10 faces the first horizontal magnet 411 b 1 of the fixed unit 30 b in the z direction.

The horizontal hall sensor hh10 may be arranged outside the spiral winding of the first horizontal coil 31 a 1 in the y direction. However, it is desirable for the horizontal hall sensor hh10 to be arranged inside the spiral winding of the first horizontal coil 31 a 1, and midway along the outer circumference of the spiral winding of the first horizontal coil 31 a 1 in the x direction (see FIG. 7).

The horizontal hall sensor hh10 is layered on the first horizontal coil 31 a 1 in the z direction. Accordingly, the area in which the magnetic field is generated for the position-detecting operation and the area in which the magnetic field is generated for driving the movable platform 30 a are shared. Therefore, the length of the first horizontal magnet 411 b 1 in the y direction and the length of the first horizontal yoke 431 b 1 in the y direction can be shortened.

The first vertical hall sensor hv1 is attached to the movable platform 30 a, where the first vertical hall sensor hv1 faces the first vertical magnet 412 b 1 of the fixed unit 30 b in the z direction.

The second vertical hall sensor hv2 is attached to the movable platform 30 a, where the second vertical hall sensor hv2 faces the second vertical magnet 412 b 2 of the fixed unit 30 b in the z direction.

The first and second vertical hall sensors hv1 and hv2 are arranged in the x direction in the initial state.

The first vertical hall sensor hv1 may be arranged outside the spiral winding of the first vertical coil 32 a 1 in the x direction. However, it is desirable for the first vertical hall sensor hv1 to be arranged inside the spiral winding of the first vertical coil 32 a 1, and midway along the outer circumference of the spiral winding of the first vertical coil 32 a 1 in the y direction.

The first vertical hall sensor hv1 is layered on the first vertical coil 32 a 1 in the z direction. Accordingly, the area in which the magnetic field is generated for the position-detecting operation and the area in which the magnetic field is generated for driving the movable platform 30 a are shared. Therefore, the length of the first vertical magnet 412 b 1 in the x direction and the length of the first vertical yoke 432 b 1 in the x direction can be shortened.

The second vertical hall sensor hv2 may be arranged outside the spiral winding of the second vertical coil 32 a 2 in the x direction. However, it is desirable for the second vertical hall sensor hv2 to be arranged inside the spiral winding of the second vertical coil 32 a 2, and midway along the outer circumference of the spiral winding of the second vertical coil 32 a 2 in the y direction.

The second vertical hall sensor hv2 is layered on the second vertical coil 32 a 2 in the z direction. Accordingly, the area in which the magnetic field is generated for the position-detecting operation and the area in which the magnetic field is generated for driving the movable platform 30 a are shared. Therefore, the length of the second vertical magnet 412 b 2 in the x direction and the length of the second vertical yoke 432 b 2 in the x direction can be shortened.

Furthermore, the first driving point to which the first vertical electro-magnetic force based on the first vertical coil 32 a 1 is applied can be close to a position-detecting point by the first vertical hall sensor hv1, and the second driving point to which the second vertical electro-magnetic force based on the second vertical coil 32 a 2 is applied can be close to a position-detecting point by the second vertical hall sensor hv2. Therefore, accurate driving control of the movable platform 30 a can be performed.

In the initial state, it is desirable for the horizontal hall sensor hh10 to be located at a place on the hall sensor unit 44 a that faces an intermediate area between the N pole and S pole of the first horizontal magnet 411 b 1 in the x direction, as viewed from the z direction, to perform the position-detecting operation utilizing the full range within which an accurate position-detecting operation can be performed based on the linear output change (linearity) of the one-axis hall sensor.

Similarly, in the initial state, it is desirable for the first vertical hall sensor hv1 to be located at a place on the hall sensor unit 44 a that faces an intermediate area between the N pole and S pole of the first vertical magnet 412 b 1 in the y direction, as viewed from the z direction.

Likewise, in the initial state, it is desirable for the second vertical hall sensor hv2 to be located at a place on the hall sensor unit 44 a that faces an intermediate area between the N pole and S pole of the second vertical magnet 412 b 2 in the y direction, as viewed from the z direction.

The first hall-sensor signal-processing unit 45 has a signal processing circuit of the magnetic-field change-detecting element that is comprised of a first hall-sensor signal-processing circuit 450, a second hall-sensor signal-processing circuit 460, and a third hall-sensor signal-processing circuit 470.

The first hall-sensor signal-processing circuit 450 detects a horizontal potential difference between the output terminals of the horizontal hall sensor hh10, based on the output signal of the horizontal hall sensor hh10.

The first hall-sensor signal-processing circuit 450 outputs the horizontal detected-position signal px to the A/D converter A/D 4 of the CPU 21, on the basis of the horizontal potential difference. The horizontal detected-position signal px represents the location of the part of the movable platform 30 a which has the horizontal hall sensor hh10, in the x direction.

The first hall-sensor signal-processing circuit 450 is connected to the horizontal hall sensor hh10 through the flexible circuit board (not depicted).

The second hall-sensor signal-processing circuit 460 detects a first vertical potential difference between the output terminals of the first vertical hall sensor hv1, based on the output signal of the first vertical hall sensor hv1.

The second hall-sensor signal-processing circuit 460 outputs the first vertical detected-position signal pyl to the A/D converter A/D 5 of the CPU 21, on the basis of the first vertical potential difference. The first vertical detected-position signal pyl represents the location of the part of the movable platform 30 a which has the first vertical hall sensor hv1 (the position-detecting point by the first vertical hall sensor hv1), in the y direction.

The second hall-sensor signal-processing circuit 460 is connected to the first vertical hall sensor hv1 through the flexible circuit board (not depicted).

The third hall-sensor signal-processing circuit 470 detects a second vertical potential difference between the output terminals of the second vertical hall sensor hv2, based on the output signal of the second vertical hall sensor hv2.

The third hall-sensor signal-processing circuit 470 outputs the second vertical detected-position signal pyr to the A/D converter A/D 6 of the CPU 21, on the basis of the second vertical potential difference. The second vertical detected-position signal pyr represents the location of the part of the movable platform 30 a which has the second vertical hall sensor hv2 (the position-detecting point by the second vertical hall sensor hv2), in the y direction.

The third hall-sensor signal-processing circuit 470 is connected to the second vertical hall sensor hv2 through the flexible circuit board (not depicted).

In the embodiment, the three hall sensors (hh10, hv1 and hv2) are used for specifying the location of the movable platform 30 a including the rotational (inclination) angle.

The locations in the y direction of the two points on the movable platform 30 a are determined by using two of the three hall sensors (hv1 and hv2). The location in the x direction of the one point on the movable platform 30 a is determined by using another of the three hall sensors (hh10). The location of the movable platform 30 a, which includes the rotational (inclination) angle in the xy plane, can be determined on the basis of the information regarding the locations in the x direction of the one point and the location in the y direction of the two points.

Next, the main operation of the photographic apparatus 1 in the embodiment is explained using the flowchart of FIG. 4.

When the PON switch 11 a is set to the ON state, the electrical power is supplied to the detection unit 25 so that the detection unit 25 is set to the ON state in step S10.

In step S11, the timer interrupt process at the predetermined time interval (1 ms) commences. In step S12, the value of the release-state parameter RP is set to 0. The details of the timer interrupt process in the embodiment are explained later using the flowchart of FIG. 5.

In step S13, the value of the holding state parameter SIS is set to 0.

In step S14, it is determined whether the photometric switch 12 a is set to the ON state. When it is determined that the photometric switch 12 a is not set to the ON state, the operation returns to step S13 and the process in steps S13 and S14 is repeated. Otherwise, the operation continues on to step S15.

In step S15, it is determined whether the correction switch 14 a is set to the ON state. When it is determined that the correction switch 14 a is not set to the ON state, the value of the correction parameter SR is set to 0 in step S16. Otherwise, the value of the correction parameter SR is set to 1 in step S17.

When the photometric switch 12 a is set to the ON state, the AE sensor of the AE unit 23 is driven, the photometric operation is performed, and the aperture value and the duration of the exposure operation are calculated, in step S18.

In step S19, the AF sensor and the lens control circuit of the AF unit 24 are driven to perform the AF sensing and focus operations, respectively. Furthermore, the lens information including the lens coefficient F is communicated from the camera lens 67 to the CPU 21.

In the photometric operation and the AF sensing operation, the result of the calculation of the holding state parameter SIS, which is performed in the timer interrupt process, is used (see step S56 in FIG. 5).

In step S20, it is determined whether the shutter release switch 13 a is set to the ON state. When the shutter release switch 13 a is not set to the ON state, the operation returns to step S13 and the process in steps S13 to S19 is repeated. Otherwise, the operation continues on to step S21.

In step S21, the value of the release-state parameter RP is set to 1, and then the release-sequence operation commences, as the initial state. In the initial state, the movable platform 30 a is positioned at the center of its movement range in both the x direction and the y direction, and each of the four sides of the rectangle composing the outline of the imaging surface of the imager 39 a 1 is parallel to either the x direction or the y direction.

In step S22, the value of the mirror state parameter MP is set to 1.

In step S23, the mirror-up operation and the aperture closing operation corresponding to the aperture value that is either preset or calculated, are performed by the mirror-aperture-shutter unit 18.

After the mirror-up operation is finished, the value of the mirror state parameter MP is set to 0, in step S24. In step S25, the opening operation of the shutter (the movement of the front curtain of the shutter) commences.

In step S26, the exposure operation, that is, the electric charge accumulation of the imager 39 a 1 (CCD etc.), is performed. After the exposure time has elapsed, the closing operation of the shutter (the movement of the rear curtain in the shutter), the mirror-down operation, and the opening operation of the aperture are performed by the mirror-aperture-shutter unit 18, in step S27.

In step S28, the value of the release-state parameter RP is set to 0 so that the photometric switch 12 a and the shutter release switch 13 a are set to the OFF state and the release-sequence operation is finished. In step S29, the electric charge accumulated in the imager 39 a 1 during the exposure time is read. In step S30, the CPU 21 communicates with the DSP 19 so that the image-processing operation is performed based on the electric charge read from the imager 39 a 1. The image on which the image-processing operation is performed is stored in the memory of the photographic apparatus 1. In step S31, the image stored in the memory is displayed on the display 17, and the operation then returns to step S13. In other words, the photographic apparatus 1 is returned to a state in which the next imaging operation can be performed.

Next, the timer interrupt process in the embodiment, which commences in step S11 in FIG. 4 and is performed at every predetermined time interval (1 ms) independent of the other operations, is explained using the flowchart of FIG. 5.

When the timer interrupt process commences, the first angular velocity vx, which is output from the detection unit 25, is input to the A/D converter A/D 0 of the CPU 21 and converted to the first digital angular velocity signal Vx_(n), in step S51. The second angular velocity vy, which is also output from the detection unit 25, is input to the A/D converter A/D 1 of the CPU 21 and converted to the second digital angular velocity signal Vy_(n) (the angular velocity detection operation).

The low frequencies of the first and second digital angular velocity signals Vx_(n) and Vy_(n) are reduced in the digital high-pass filtering (the first and second digital angular velocities VVx_(n) and VVy_(n), see (1) in FIG. 6).

When the timer interrupt process commences, the Lo signal is output from port P10 of the CPU 21.

In step S52, the hall sensor unit 44 a detects the position of the movable platform 30 a. The horizontal detected-position signal px and the first and second vertical detected-position signals pyl and pyr are calculated by the hall-sensor signal-processing unit 45. The horizontal detected-position signal px is then input to the A/D converter A/D 4 of the CPU 21 and converted to the digital signal pdx_(n), the first vertical detected-position signal pyl is then input to the A/D converter A/D 5 of the CPU 21 and converted to the digital signal pdyl_(n), and the second vertical detected-position signal pyr is input to the A/D converter A/D 6 of the CPU 21 and also converted to the digital signal pdyr_(n), both of which thus specify the present position P_(n) (pdx_(n), pdyl_(n), pdyr_(n)) of the movable platform 30 a (see (2) in FIG. 6).

In step S53, it is determined whether the value of the release-state parameter RP is set to 1. When it is determined that the value of the release-state parameter RP is not set to 1, the operation continues to step S54, otherwise, the operation proceeds to step S59.

In step S54, the output signal from port P10 of the CPU 21 is changed from the Lo signal to the Hi signal.

In step S55, the first acceleration ah, which is also output from the detection unit 25, is input to the A/D converter A/D 2 of the CPU 21 and converted to the first digital acceleration signal Dah_(n). Similarly, the second acceleration av, which is also output from the detection unit 25, is input to the A/D converter A/D 3 of the CPU 21 and converted to the second digital acceleration signal Dav_(n) (the acceleration detection operation).

In the acceleration detection operation in step S55, the first acceleration ah and the second acceleration av, which are amplified with the low amplification rate Am2 by the third and fourth amplifiers 28 c and 28 d corresponding to the Hi signal output from port P10 of the CPU 21, are input to the CPU 21.

The high frequencies of the first and second digital acceleration signals Dah_(n) and Dav_(n) are reduced in the digital low-pass filtering (the first and second digital acceleration Aah_(n) and Aav_(n), see (1) in FIG. 6).

In step S56, the holding state of the photographic apparatus 1 is specified, in other words, the calculation of the holding state parameter SIS is performed. The details of the calculation of the holding state parameter SIS in the embodiment are explained later using the flowchart of FIG. 17.

In step S57, the output signal from port P10 of the CPU 21 is changed from the Hi signal to the Lo signal.

In step S58, driving the movable platform 30 a is set to the OFF state, in other words, the correction unit 30 is set to a state where the driving control of the movable platform 30 a is not performed.

In step S59, the first acceleration ah, which is also output from the detection unit 25, is input to the A/D converter A/D 2 of the CPU 21 and converted to the first digital acceleration signal Dah_(n). Similarly, the second acceleration av, which is also output from the detection unit 25, is input to the A/D converter A/D 3 of the CPU 21 and converted to the second digital acceleration signal Dav_(n) (the acceleration detection operation).

In the acceleration detection operation in step S59, the first acceleration ah and the second acceleration av, which are amplified with the high amplification rate Am1 by the third and fourth amplifiers 28 c and 28 d corresponding to the Lo signal output from port P10 of the CPU 21, are input to the CPU 21.

The high frequencies of the first and second digital acceleration signals Dah_(n) and Dav_(n) are reduced in the digital low-pass filtering (the first and second digital acceleration Aah_(n) and Aav_(n), see (1) in FIG. 6).

In step S60, it is determined whether the value of the correction parameter SR is 0. When it is determined that the value of the correction parameter SR is 0 (SR=0), in other words, that the photographic apparatus 1 is not in the correction mode, the position S_(n) (Sx_(n), Syl_(n), Syr_(n)) where the movable platform 30 a should be moved, is set to the initial state (Sx_(n)=Syl_(n)=Syr_(n)=0) in step S61 (see (4) in FIG. 6).

When it is determined that the value of the correction parameter SR is not 0 (SR=1), in other words when the photographic apparatus 1 is in correction mode, the operation continues to step S62, in order to perform the first and second stabilizations.

In step S62, the third digital displacement angle Kθ_(n) is calculated on the basis of the first and second digital accelerations Aah_(n) and Aav_(n) (see (8) in FIG. 6).

The details of the calculation of the third digital displacement angle Kθ_(n) in the embodiment are explained later using the flowchart of FIG. 8.

In step S63, the rotational (inclination) direction component of the position S_(n), Sθ_(n), is calculated on the basis of the third digital displacement angle Kθ_(n) and the hall sensor distance coefficient HSD (see (3) in FIG. 6).

In step S64, the first and second digital displacement angles Kx_(n) and Ky_(n) are calculated on the basis of the first and second digital angular velocities VVx_(n) and VVy_(n) (see (7) in FIG. 6).

In step S65, the horizontal direction component of the position S_(n), Sx_(n), and the vertical direction component of the position S_(n), Sy_(n), are calculated on the basis of the first digital displacement angle Kx_(n), the second digital displacement angle Ky_(n), and the lens coefficient F (see (3) in FIG. 6).

Then, the first vertical direction component of the first driving point Syl_(n) and the second vertical direction component of the second driving point Syr_(n) are calculated on the basis of the vertical direction component of the position S_(n), Sy_(n), and the rotational (inclination) direction component of the position S_(n), Sθ_(n) (see (4) in FIG. 6).

In step S66, the horizontal driving force Dx_(n) (the horizontal PWM duty dx), the first vertical driving force Dyl_(n) (the first vertical PWM duty dyl), and the second vertical driving force Dyr_(n) (the second vertical PWM duty dyr) of the driving force D_(n), which moves the movable platform 30 a to the position S_(n), are calculated on the basis of the position S_(n) (Sx_(n), Sy_(n), Sθ_(n)) that was determined in step S61 or step S65, and the present position P_(n) (pdx_(n), pdyl_(n), pdyr_(n)) (see (5) in FIG. 6).

In step S67, the first and second horizontal coils 31 a 1 and 31 a 2 are driven by applying the horizontal PWM duty dx to the driver circuit 29; the first vertical coil 32 a 1 is driven by applying the first vertical PWM duty dyl to the driver circuit 29; and the second vertical coil 32 a 2 is driven by applying the second vertical PWM duty dyr to the driver circuit 29, so that the movable platform 30 a is moved to position S_(n) (Sx_(n), Sy_(n), Sθ_(n)) (see (6) in FIG. 6).

The process of steps S66 and S67 is an automatic control calculation that is performed by the PID automatic control for performing general (normal) proportional, integral, and differential calculations.

Next, the calculation of the third digital displacement angle Kθ_(n), which is performed in step S62 in FIG. 5, is explained using the flowchart of FIG. 8.

When the calculation of the third digital displacement angle Kθ_(n) commences, it is determined whether the absolute value of the second digital acceleration Aav_(n) is larger than or equal to the absolute value of the first digital acceleration Aah_(n), in step S71.

When it is determined that the absolute value of the second digital acceleration Aav_(n) is larger than or equal to the absolute value of the first digital acceleration Aah_(n), the operation proceeds to step S75, otherwise, the operation continues to step S72.

In step S72, it is determined whether the first digital acceleration Aah_(n) is less than 0. When it is determined that the first digital acceleration Aah_(n) is less than 0, the operation proceeds to step S74, otherwise, the operation continues to step S73.

In step S73, the CPU 21 determines that the photographic apparatus 1 is held approximately in the first vertical orientation, and calculates the inclination angle (the third digital displacement angle Kθ_(n)) by performing the arcsine transformation on the second digital acceleration Aav_(n) and taking the negative (Kθ_(n)=−Sin⁻¹(Aav_(n))).

In step S74, the CPU 21 determines that the photographic apparatus is held approximately in the second vertical orientation, and calculates the inclination angle (the third digital displacement angle Kθ_(n)) by performing the arcsine transformation on the second digital acceleration Aav_(n) (Kθ_(n)=+Sin⁻¹(Aav_(n))).

In step S75, it is determined whether the second digital acceleration Aav_(n) is less than 0. When it is determined that the second digital acceleration Aav_(n) is less than 0, the operation proceeds to step S77, otherwise, the operation continues to step S76.

In step S76, the CPU 21 determines that the photographic apparatus 1 is held approximately in the first horizontal orientation, and calculates the inclination angle (the third digital displacement angle Kθ_(n)) by performing the arcsine transformation on the first digital acceleration Aah_(n) (Kθ_(n)=+Sin⁻¹(Aah_(n))).

In step S77, the CPU 21 determines that the photographic apparatus is held approximately in the second horizontal orientation, and calculates the inclination angle (the third digital displacement angle Kθ_(n)) by performing the arcsine transformation on the first digital acceleration Aah_(n) and taking the negative (Kθ_(n)=−sin⁻¹(Aah_(n))).

Next, the calculation of the holding state parameter SIS, which is performed in step S56 in FIG. 5, is explained using the flowchart of FIG. 17.

When the calculation of the holding state parameter SIS commences, it is determined whether the absolute value of the second digital acceleration Aav_(n) is larger than or equal to the absolute value of the first digital acceleration Aah_(n), in step S91.

When it is determined that the absolute value of the second digital acceleration Aav_(n) is larger than or equal to the absolute value of the first digital acceleration Aah_(n), the operation proceeds to step S95, otherwise, the operation continues to step S92.

In step S92, it is determined whether the first digital acceleration Aah_(n) is less than 0. When it is determined that the first digital acceleration Aah_(n) is less than 0, the operation proceeds to step S94, otherwise, the operation continues to step S93.

In step S93, the CPU 21 determines that the photographic apparatus 1 is held approximately in the first vertical orientation, and the value of the holding state parameter SIS is set to 2.

In step S94, the CPU 21 determines that the photographic apparatus is held approximately in the second vertical orientation, and the value of the holding state parameter SIS is set to 3.

In step S95, it is determined whether the second digital acceleration Aav_(n) is less than 0. When it is determined that the second digital acceleration Aav_(n) is less than 0, the operation proceeds to step S97, otherwise, the operation continues to step S96.

In step S96, the CPU 21 determines that the photographic apparatus 1 is held approximately in the first horizontal orientation, and the value of the holding state parameter SIS is set to 0.

In step S97, the CPU 21 determines that the photographic apparatus is held approximately in the second horizontal orientation, and the value of the holding state parameter SIS is set to 1.

Therefore, the calculation except for during the release sequence operation (RP=0) can be simplified, because the accurate inclination angle for the inclination correction is not calculated.

Furthermore, it is explained that the hall sensor is used for position detection as the magnetic-field change-detecting element. However, another detection element, an MI (Magnetic Impedance) sensor such as a high-frequency carrier-type magnetic-field sensor, a magnetic resonance-type magnetic-field detecting element, or an MR (Magneto-Resistance effect) element may be used for position detection purposes. When one of either the MI sensor, the magnetic resonance-type magnetic-field detecting element, or the MR element is used, the information regarding the position of the movable platform can be obtained by detecting the magnetic-field change, similar to using the hall sensor.

Although the embodiment of the present invention has been described herein with reference to the accompanying drawings, obviously many modifications and changes may be made by those skilled in this art without departing from the scope of the invention.

The present disclosure relates to subject matter contained in Japanese Patent Application No. 2008-095700 (filed on Apr. 2, 2008), which is expressly incorporated herein by reference, in its entirety. 

1. A photographic apparatus comprising: a movable platform which has an imager that captures an optical image through a taking lens, and is movable and rotatable in an xy plane perpendicular to an optical axis of said taking lens; an acceleration sensor that detects a first gravitational component and a second gravitational component, said first gravitational component being a component of gravitational acceleration in an x direction perpendicular to said optical axis, and said second gravitational component being a component of gravitational acceleration in a y direction perpendicular to said optical axis and said x direction; and a controller that specifies a holding state of said photographic apparatus, calculates an inclination angle of said photographic apparatus formed by rotation of said photographic apparatus around said optical axis, as measured with respect to a level plane perpendicular to a direction of gravitational force, on the basis of said first gravitational component and said second gravitational component, and performs a movement control of said movable platform for an inclination correction based on said inclination angle; said controller specifying said holding state before an imaging operation by said imager that commences when a shutter release switch is set to an ON state, and performing said inclination correction during said imaging operation, wherein a detection resolution of an A/D conversion of said first and second gravitational components when said controller performs said inclination correction, is greater than a detection resolution of an A/D conversion of said first and second gravitational components when said controller specifies said holding state.
 2. The photographic apparatus according to claim 1, wherein an amplification rate of said first and second gravitational components when said controller performs said inclination correction, is greater than an amplification rate of said first and second gravitational components when said controller specifies said holding state.
 3. The photographic apparatus according to claim 1, wherein information regarding said holding state is used for at least one of a photometric operation of said photographic apparatus and an AF sensing operation of said photographic apparatus.
 4. The photographic apparatus according to claim 1, wherein information regarding said holding state is attached to a file storing an image obtained by said imaging operation.
 5. The photographic apparatus according to claim 1, wherein said controller specifies said holding state and performs said inclination correction, on the basis of a magnitude relation between the absolute value of said first gravitational component and the absolute value of said second gravitational component.
 6. The photographic apparatus according to claim 1, wherein said x direction is perpendicular to the direction of gravitational force and said y direction is parallel to the direction of gravitational force when said photographic apparatus is held horizontally and either an upper surface or a lower surface of said photographic apparatus faces upward; and said x direction is parallel to the direction of gravitational force and said y direction is perpendicular to the direction of gravitational force when said photographic apparatus is held vertically and one of either side surfaces of said photographic apparatus faces upward. 